FR2973829B1 - Flasque d'etancheite pour etage de turbine de turbomachine d'aeronef, comprenant - Google Patents
Flasque d'etancheite pour etage de turbine de turbomachine d'aeronef, comprenantInfo
- Publication number
- FR2973829B1 FR2973829B1 FR1152928A FR1152928A FR2973829B1 FR 2973829 B1 FR2973829 B1 FR 2973829B1 FR 1152928 A FR1152928 A FR 1152928A FR 1152928 A FR1152928 A FR 1152928A FR 2973829 B1 FR2973829 B1 FR 2973829B1
- Authority
- FR
- France
- Prior art keywords
- turbine
- rotor disc
- aircraft
- sealing plate
- ring
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/005—Sealing means between non relatively rotating elements
- F01D11/006—Sealing the gap between rotor blades or blades and rotor
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
- F01D5/3007—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
- F01D5/3015—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type with side plates
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/005—Sealing means between non relatively rotating elements
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
- F01D5/32—Locking, e.g. by final locking blades or keys
- F01D5/323—Locking of axial insertion type blades by means of a key or the like parallel to the axis of the rotor
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/30—Retaining components in desired mutual position
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/60—Fluid transfer
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49995—Shaping one-piece blank by removing material
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Priority Applications (8)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1152928A FR2973829B1 (fr) | 2011-04-05 | 2011-04-05 | Flasque d'etancheite pour etage de turbine de turbomachine d'aeronef, comprenant |
BR112013025486-6A BR112013025486B1 (pt) | 2011-04-05 | 2012-03-29 | Anel de vedação para ser prensado contra um disco de rotor de umestágio de turbina para uma turbomáquina de avião e método para fabricar omesmo |
US14/009,302 US9494042B2 (en) | 2011-04-05 | 2012-03-29 | Sealing ring for a turbine stage of an aircraft turbomachine, comprising slotted anti-rotation pegs |
PCT/FR2012/050667 WO2012136917A1 (fr) | 2011-04-05 | 2012-03-29 | Flasque d'etancheite pour etage de turbine de turbomachine d'aeronef, comprenant des tenons anti-rotation fendus |
CA2831522A CA2831522C (fr) | 2011-04-05 | 2012-03-29 | Flasque d'etancheite pour etage de turbine de turbomachine d'aeronef, comprenant des tenons anti-rotation fendus |
CN201280017127.3A CN103459777B (zh) | 2011-04-05 | 2012-03-29 | 用于航空器涡轮机组的涡轮机级的密封圈,包括开狭槽的防旋转栓 |
RU2013148796/06A RU2594392C2 (ru) | 2011-04-05 | 2012-03-29 | Уплотнительное кольцо для ступени турбины турбомашины летательного аппарата, содержащее запорные выступы с прорезями, ротор ступени турбомашины, турбомашина и способ изготовления уплотнительного кольца |
EP12717412.6A EP2694781B1 (fr) | 2011-04-05 | 2012-03-29 | Flasque d'etancheite pour etage de turbine de turbomachine d'aeronef, comprenant des tenons anti-rotation fendus |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1152928A FR2973829B1 (fr) | 2011-04-05 | 2011-04-05 | Flasque d'etancheite pour etage de turbine de turbomachine d'aeronef, comprenant |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2973829A1 FR2973829A1 (fr) | 2012-10-12 |
FR2973829B1 true FR2973829B1 (fr) | 2013-05-24 |
Family
ID=46017971
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1152928A Expired - Fee Related FR2973829B1 (fr) | 2011-04-05 | 2011-04-05 | Flasque d'etancheite pour etage de turbine de turbomachine d'aeronef, comprenant |
Country Status (8)
Country | Link |
---|---|
US (1) | US9494042B2 (pt) |
EP (1) | EP2694781B1 (pt) |
CN (1) | CN103459777B (pt) |
BR (1) | BR112013025486B1 (pt) |
CA (1) | CA2831522C (pt) |
FR (1) | FR2973829B1 (pt) |
RU (1) | RU2594392C2 (pt) |
WO (1) | WO2012136917A1 (pt) |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3026430B1 (fr) * | 2014-09-29 | 2020-07-10 | Safran Aircraft Engines | Roue de turbine dans une turbomachine |
US10215043B2 (en) | 2016-02-24 | 2019-02-26 | United Technologies Corporation | Method and device for piston seal anti-rotation |
FR3049307B1 (fr) * | 2016-03-25 | 2019-11-01 | Safran Aircraft Engines | Ensemble rotatif pour turbomachine |
EP3521561A1 (de) * | 2018-02-02 | 2019-08-07 | Siemens Aktiengesellschaft | Rotor mit dichtelement und dichtring |
US11105424B2 (en) | 2019-02-01 | 2021-08-31 | Kaydon Ring & Seal, Inc. | Crowned anti-rotation device for circumferential seals |
US11313240B2 (en) * | 2020-02-05 | 2022-04-26 | Raytheon Technologies Corporation | Rounded radial snap configuration for a gas turbine engine cover plate |
CN114810220B (zh) * | 2021-01-29 | 2024-02-20 | 中国航发商用航空发动机有限责任公司 | 航空发动机 |
Family Cites Families (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3266770A (en) * | 1961-12-22 | 1966-08-16 | Gen Electric | Turbomachine rotor assembly |
FR2393931A1 (fr) * | 1977-06-08 | 1979-01-05 | Snecma | Dispositif de maintien des aubes d'un rotor |
FR2585069B1 (fr) * | 1985-07-16 | 1989-06-09 | Snecma | Dispositif de limitation du debattement angulaire d'aubes montees sur un disque de rotor de turbomachine |
FR2666623B1 (fr) * | 1990-09-11 | 1993-05-07 | Turbomeca | Roue de turbomachine a pales rapportees. |
US5211407A (en) * | 1992-04-30 | 1993-05-18 | General Electric Company | Compressor rotor cross shank leak seal for axial dovetails |
FR2695433B1 (fr) * | 1992-09-09 | 1994-10-21 | Snecma | Joint annulaire d'étanchéité disposé à une extrémité axiale d'un rotor et recouvrant des brochages d'aubes. |
US5318405A (en) * | 1993-03-17 | 1994-06-07 | General Electric Company | Turbine disk interstage seal anti-rotation key through disk dovetail slot |
US6190131B1 (en) * | 1999-08-31 | 2001-02-20 | General Electric Co. | Non-integral balanced coverplate and coverplate centering slot for a turbine |
GB9925261D0 (en) * | 1999-10-27 | 1999-12-29 | Rolls Royce Plc | Locking devices |
US6464453B2 (en) * | 2000-12-04 | 2002-10-15 | General Electric Company | Turbine interstage sealing ring |
FR2850130B1 (fr) * | 2003-01-16 | 2006-01-20 | Snecma Moteurs | Dispositif pour retenir un flasque annulaire contre une face radiale d'un disque |
US7721433B2 (en) * | 2005-03-28 | 2010-05-25 | United Technologies Corporation | Blade outer seal assembly |
US7500832B2 (en) * | 2006-07-06 | 2009-03-10 | Siemens Energy, Inc. | Turbine blade self locking seal plate system |
CN200943509Y (zh) * | 2006-07-26 | 2007-09-05 | 沈阳黎明航空发动机(集团)有限责任公司 | 一种径向销钉连接的透平盘 |
ATE441776T1 (de) * | 2007-01-09 | 2009-09-15 | Siemens Ag | Axialer rotorabschnitt für einen rotor einer turbine |
FR2913064B1 (fr) * | 2007-02-22 | 2009-04-10 | Snecma Sa | Flasque annulaire d'etancheite pour disque de rotor dans une turbomachine |
FR2918103B1 (fr) * | 2007-06-27 | 2013-09-27 | Snecma | Dispositif de refroidissement des alveoles d'un disque de rotor de turbomachine. |
FR2922589B1 (fr) * | 2007-10-22 | 2009-12-04 | Snecma | Controle du jeu en sommet d'aubes dans une turbine haute-pression de turbomachine |
EP2182170A1 (de) * | 2008-10-30 | 2010-05-05 | Siemens Aktiengesellschaft | Gasturbine mit Dichtplatten an der Turbinenscheibe |
US8459953B2 (en) * | 2010-01-19 | 2013-06-11 | General Electric Company | Seal plate and bucket retention pin assembly |
-
2011
- 2011-04-05 FR FR1152928A patent/FR2973829B1/fr not_active Expired - Fee Related
-
2012
- 2012-03-29 CN CN201280017127.3A patent/CN103459777B/zh active Active
- 2012-03-29 RU RU2013148796/06A patent/RU2594392C2/ru active
- 2012-03-29 WO PCT/FR2012/050667 patent/WO2012136917A1/fr active Application Filing
- 2012-03-29 BR BR112013025486-6A patent/BR112013025486B1/pt active IP Right Grant
- 2012-03-29 CA CA2831522A patent/CA2831522C/fr active Active
- 2012-03-29 EP EP12717412.6A patent/EP2694781B1/fr active Active
- 2012-03-29 US US14/009,302 patent/US9494042B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
CA2831522C (fr) | 2018-06-12 |
US20150159496A1 (en) | 2015-06-11 |
FR2973829A1 (fr) | 2012-10-12 |
CN103459777A (zh) | 2013-12-18 |
CN103459777B (zh) | 2015-04-15 |
RU2594392C2 (ru) | 2016-08-20 |
CA2831522A1 (fr) | 2012-10-11 |
WO2012136917A1 (fr) | 2012-10-11 |
US9494042B2 (en) | 2016-11-15 |
EP2694781A1 (fr) | 2014-02-12 |
BR112013025486B1 (pt) | 2021-02-23 |
RU2013148796A (ru) | 2015-05-10 |
EP2694781B1 (fr) | 2015-01-14 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PLFP | Fee payment |
Year of fee payment: 5 |
|
ST | Notification of lapse |
Effective date: 20161230 |